US3942847A - Temperature compensating ceramic metal bearing systems - Google Patents
Temperature compensating ceramic metal bearing systems Download PDFInfo
- Publication number
- US3942847A US3942847A US05/434,645 US43464574A US3942847A US 3942847 A US3942847 A US 3942847A US 43464574 A US43464574 A US 43464574A US 3942847 A US3942847 A US 3942847A
- Authority
- US
- United States
- Prior art keywords
- temperature compensating
- ceramic member
- bearing
- bearing assembly
- helical
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000919 ceramic Substances 0.000 title claims abstract description 26
- 239000002184 metal Substances 0.000 title description 4
- 229910052751 metal Inorganic materials 0.000 title description 4
- 229910052581 Si3N4 Inorganic materials 0.000 claims description 10
- HQVNEWCFYHHQES-UHFFFAOYSA-N silicon nitride Chemical compound N12[Si]34N5[Si]62N3[Si]51N64 HQVNEWCFYHHQES-UHFFFAOYSA-N 0.000 claims description 10
- 239000000463 material Substances 0.000 claims description 5
- 238000007789 sealing Methods 0.000 claims description 4
- 239000007789 gas Substances 0.000 description 11
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 239000007769 metal material Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 2
- 229910002804 graphite Inorganic materials 0.000 description 2
- 239000010439 graphite Substances 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000005086 pumping Methods 0.000 description 2
- 238000009718 spray deposition Methods 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000011888 foil Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 230000013011 mating Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 239000011863 silicon-based powder Substances 0.000 description 1
- 230000002889 sympathetic effect Effects 0.000 description 1
- 230000008646 thermal stress Effects 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C17/00—Sliding-contact bearings for exclusively rotary movement
- F16C17/12—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load
- F16C17/22—Sliding-contact bearings for exclusively rotary movement characterised by features not related to the direction of the load with arrangements compensating for thermal expansion
Definitions
- This invention relates to temperature compensating bearing assemblies and in particular to temperature compensating ceramic/metal bearing assemblies.
- the present invention relates to a temperature compensating bearing for a shaft or a like movable member in which an expandible helical ceramic member is employed intermediate between the shaft and a housing therefor.
- the invention When the invention is applied to a dry bearing assembly required to operate over a wide temperature range it may include a graphitic material located within the space provided by the gap in the expandible helical ceramic member, which graphitic material will then be dispursed over the bearing surfaces during operation if the bearing as a lubricating film of graphite.
- the expandible helical ceramic member is preferably of silicon nitride and may be fabricated by any of the known fabrication techniques.
- FIG. 1 is a perspective view of the ceramic helical member
- FIG. 2 illustrates a bearing in accordance with the present invention
- FIG. 3 is a perspective view of a modified shaft.
- an expandible helical ceramic member 1 is designed to operate by expanding and contracting sympathetically with change in shaft diameter with change in temperature whilst maintaining gas clearances with the bearing surfaces on the metal housing 2.
- the helical gap 3 formed in the helical ceramic member 1 acts also to assist to even out the gas pressure in the bearing and also provide a degree of pumping action.
- This pumping action can be further enhanced by forming a counter helical groove 4 in the shaft 5, as shown in FIG. 3. It is necessary to provide end sealing arrangements to the bearing, in order to maintain gas pressures within the bearing demanded by the required bearing stiffness, and cover plates 6 fitting close to the surface of the shaft to restrict gas flow are provided for that purpose.
- separate split collars with close tolerances can be provided at each end of the bearing, as described in U.S. Pat. No. 1,310,274.
- the helical ceramic member may be formed of silicon nitride by the flame-spray deposition of fine silicon powder onto a polished mandrel previously coated with a soluble release agent, as described in U.S. Pat. No. 1,138,284.
- the helix is then ground externally, whilst still on the mandrel, and is then released and reaction bonded to silicon nitride by heating in nitrogen and then lightly finished to final dimensions by polishing.
- the circumferential shots 7 in the helix may be made by stretching thin foil (eg 0.0001 inch) between sets of removable split pegs fitted into the mandrel before spray deposition.
- the bearing may be self-pressurised due to the counter helical groove in the shaft, assisted by the helical gap in the ceramic helix, or jacking gas may be supplied to the bearing through a conduit 8 passing through the housing.
- the invention may be used in a modified form for use in rotational or reciprocating shaft dry journal bearings to operate over wide temperature ranges, particularly if a graphic spiral for dispensing graphite films over the surface of the shaft is enclosed in the space provided by the gap in the ceramic helix.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sliding-Contact Bearings (AREA)
- Ceramic Products (AREA)
- Support Of The Bearing (AREA)
Abstract
The invention concerns a temperature compensating bearing for a shaft in which an expandable helical ceramic member is provided between the shaft and the bearing housing. The expandable helical ceramic member functions by expanding and contracting sympathetically with any changes in shaft diameter due to change of temperature of the bearing.
Description
This invention relates to temperature compensating bearing assemblies and in particular to temperature compensating ceramic/metal bearing assemblies.
An alleviation of strict design and operating criteria for bearing technology by the use of inorganic non-metallic to metallic mating surfaces in critical components of bearing systems has been described in British Pat. No. 1,310,274. The precise choice of metallic and inorganic non-metallic components depends upon operating loads, speeds and invironments, but where high temperatures are involved the preferred inorganic non-metallic material must have a combination of high temperature strength, low co-efficient of friction and high resistance to fracture by thermal stress or thermal shock. Such properties are obtainable in reaction-bonded or hotpressed silicon nitride and its derivatives.
One of the chief virtues of using such combinations of materials in gas bearing technology is to permit fortuitous touch-down without causing catastrophic failure by seizing or galling as is normal to total metallic systems. The use of inorganic non-metallic materials with metals will thus permit the possibility of a bearing operation passing from a plain journal unlubricated system to a self-pressurised gas bearing system as shaft speed is increased with or without the use of jacking gas.
The chief problems attendant with the use of mixed metallic/inorganic non-metallic materials in systems expected to operate over temperature ranges is the inherent difference in co-efficients of thermal expansion. In order, therefore, to avoid loss of close tolerance of clearances, or to avoid fracture loads imposed by thermal expansion mismatch, it is necessary to provide means for the sympathetic compensation of dimension changes consequent upon temperature gradients and levels.
The present invention relates to a temperature compensating bearing for a shaft or a like movable member in which an expandible helical ceramic member is employed intermediate between the shaft and a housing therefor.
When the invention is applied to gas bearing assemblies it is very desirable to provide end sealing covers on plates which are arranged to fit closely around the shaft to restrict the loss of gas pressure from within the bearing of gas pressure from within the bearing assembly. Presurisation of the bearing assembly may with advantage be aided by the provision on the bearing surface of the shaft of a helical groove arranged in counterdirection to the helix angle of the expandible helical ceramic member.
When the invention is applied to a dry bearing assembly required to operate over a wide temperature range it may include a graphitic material located within the space provided by the gap in the expandible helical ceramic member, which graphitic material will then be dispursed over the bearing surfaces during operation if the bearing as a lubricating film of graphite.
The expandible helical ceramic member is preferably of silicon nitride and may be fabricated by any of the known fabrication techniques.
In order that the present invention may be more fully understood embodiments thereof will now be described, by way of example, with reference to the accompanying drawings, in which:
FIG. 1 is a perspective view of the ceramic helical member;
FIG. 2 illustrates a bearing in accordance with the present invention; and
FIG. 3 is a perspective view of a modified shaft.
Referring to the drawings, an expandible helical ceramic member 1 is designed to operate by expanding and contracting sympathetically with change in shaft diameter with change in temperature whilst maintaining gas clearances with the bearing surfaces on the metal housing 2. The helical gap 3 formed in the helical ceramic member 1 acts also to assist to even out the gas pressure in the bearing and also provide a degree of pumping action. This pumping action can be further enhanced by forming a counter helical groove 4 in the shaft 5, as shown in FIG. 3. It is necessary to provide end sealing arrangements to the bearing, in order to maintain gas pressures within the bearing demanded by the required bearing stiffness, and cover plates 6 fitting close to the surface of the shaft to restrict gas flow are provided for that purpose. Alternatively, separate split collars with close tolerances can be provided at each end of the bearing, as described in U.S. Pat. No. 1,310,274.
The helical ceramic member may be formed of silicon nitride by the flame-spray deposition of fine silicon powder onto a polished mandrel previously coated with a soluble release agent, as described in U.S. Pat. No. 1,138,284. The helix is then ground externally, whilst still on the mandrel, and is then released and reaction bonded to silicon nitride by heating in nitrogen and then lightly finished to final dimensions by polishing. The circumferential shots 7 in the helix may be made by stretching thin foil (eg 0.0001 inch) between sets of removable split pegs fitted into the mandrel before spray deposition. The bearing may be self-pressurised due to the counter helical groove in the shaft, assisted by the helical gap in the ceramic helix, or jacking gas may be supplied to the bearing through a conduit 8 passing through the housing.
The invention may be used in a modified form for use in rotational or reciprocating shaft dry journal bearings to operate over wide temperature ranges, particularly if a graphic spiral for dispensing graphite films over the surface of the shaft is enclosed in the space provided by the gap in the ceramic helix.
Further specific fabrication techniques for producing silicon nitride bodies that are applicable to the fabrication of the expandible helical ceramic member are described in British Pat. No. 1,021,053 and pending British Pat. No. 52445/72.
Claims (11)
1. A temperature compensating bearing assembly for a shaft comprising a bearing housing, and an expandable helical ceramic member located within said bearing housing and providing a bearing surface.
2. A temperature compensating bearing assembly as claimed in claim 1 in which the expandable helical ceramic member is fabricated from silicon nitride.
3. A temperature compensating bearing assembly as claimed in claim 1 in which said bearing surface is comprised in part of the expandable helical ceramic member and in part of a helical spiral of graphitic material, said helical spiral of graphitic material being located in the helical spiral of the expandable helical ceramic member.
4. A temperature compensating bearing assembly as claimed in claim 3 in which the expandable helical ceramic member is fabricated from silicon nitride.
5. A temperature compensating bearing assembly comprising an expandable helical ceramic member located within said bearing housing and providing a first opposed bearing surface and a shaft located within said expandable helical ceramic member and including a second opposed bearing surface opposed to said first bearing surface.
6. A temperature compensating bearing assembly as claimed in claim 5 in which said second opposed bearing surface includes a helical groove arranged in an angled direction in counter-direction to the helix angle of the expandable helical ceramic member.
7. A temperature compensating bearing assembly as claimed in claim 5 including end sealing cover plates located at the ends of the bearing housing and arranged to fit closely around the shaft.
8. A temperature compensating bearing assembly as claimed in claim 6 including end sealing cover plates located at the end of the bearing housing and arranged to fit closely around the shaft.
9. A temperature compensating bearing assembly as claimed in claim 5 in which the expandable helical ceramic member is fabricated from silicon nitride.
10. A temperature compensating bearing assembly as claimed in claim 6 in which the expandable helical ceramic member is fabricated from silicon nitride.
11. A temperature compensating bearing assembly as claimed in claim 7 in which the expandable helical ceramic member is fabricated from silicon nitride.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UK2780/73 | 1973-01-19 | ||
GB278073A GB1417244A (en) | 1973-01-19 | 1973-01-19 | Temperature compensating ceramic/metal bearing assemblies |
Publications (1)
Publication Number | Publication Date |
---|---|
US3942847A true US3942847A (en) | 1976-03-09 |
Family
ID=9745762
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US05/434,645 Expired - Lifetime US3942847A (en) | 1973-01-19 | 1974-01-18 | Temperature compensating ceramic metal bearing systems |
Country Status (3)
Country | Link |
---|---|
US (1) | US3942847A (en) |
DE (1) | DE2402382A1 (en) |
GB (1) | GB1417244A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5947610A (en) * | 1997-11-19 | 1999-09-07 | Danieli Wean | Hydrodynamic thrust bearing assembly |
US6135641A (en) * | 1997-10-30 | 2000-10-24 | Honeywell International Inc. | Hybrid duplex bearing assembly having thermal compensation |
US20090148274A1 (en) * | 2007-12-07 | 2009-06-11 | Kostka Richard A | Compact bearing support |
US20120288368A1 (en) * | 2009-12-10 | 2012-11-15 | Hitachi, Ltd. | Slide bearing device and compressor |
CN103302293A (en) * | 2013-05-24 | 2013-09-18 | 淮海工学院 | Spray deposition densifying device and application thereof |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6191067A (en) * | 1984-10-10 | 1986-05-09 | 株式会社東芝 | Sliding member |
DE9001227U1 (en) * | 1990-02-03 | 1990-04-05 | H. Krantz Gmbh & Co, 52072 Aachen | Combination profile |
FR2710114B1 (en) * | 1993-09-17 | 1995-11-17 | Renault | Hydrodynamic bearing bushing for internal combustion engine. |
GB9418973D0 (en) * | 1994-09-21 | 1994-11-09 | Rolls Royce Power Eng | Bearing assembly |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1204042A (en) * | 1958-10-03 | 1960-01-22 | Self-lubricating guide ring | |
US3150822A (en) * | 1961-02-09 | 1964-09-29 | Commissariat Energie Atomique | Sealing and centering device for rotary shaft |
US3194616A (en) * | 1962-01-29 | 1965-07-13 | Saurer Ag Adolph | Gas lubricated sleeve bearing for gas turbines |
US3238000A (en) * | 1962-09-06 | 1966-03-01 | Philips Corp | Radial sliding bearing for traversing shafts |
US3284144A (en) * | 1964-06-08 | 1966-11-08 | American Lava Corp | Bearings |
US3494674A (en) * | 1967-03-31 | 1970-02-10 | Philips Corp | Hydrodynamic bearing for axial and radial loads |
-
1973
- 1973-01-19 GB GB278073A patent/GB1417244A/en not_active Expired
-
1974
- 1974-01-18 US US05/434,645 patent/US3942847A/en not_active Expired - Lifetime
- 1974-01-18 DE DE2402382A patent/DE2402382A1/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1204042A (en) * | 1958-10-03 | 1960-01-22 | Self-lubricating guide ring | |
US3150822A (en) * | 1961-02-09 | 1964-09-29 | Commissariat Energie Atomique | Sealing and centering device for rotary shaft |
US3194616A (en) * | 1962-01-29 | 1965-07-13 | Saurer Ag Adolph | Gas lubricated sleeve bearing for gas turbines |
US3238000A (en) * | 1962-09-06 | 1966-03-01 | Philips Corp | Radial sliding bearing for traversing shafts |
US3284144A (en) * | 1964-06-08 | 1966-11-08 | American Lava Corp | Bearings |
US3494674A (en) * | 1967-03-31 | 1970-02-10 | Philips Corp | Hydrodynamic bearing for axial and radial loads |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6135641A (en) * | 1997-10-30 | 2000-10-24 | Honeywell International Inc. | Hybrid duplex bearing assembly having thermal compensation |
US5947610A (en) * | 1997-11-19 | 1999-09-07 | Danieli Wean | Hydrodynamic thrust bearing assembly |
US20090148274A1 (en) * | 2007-12-07 | 2009-06-11 | Kostka Richard A | Compact bearing support |
US7857519B2 (en) | 2007-12-07 | 2010-12-28 | Pratt & Whitney Canada Corp. | Compact bearing support |
US20120288368A1 (en) * | 2009-12-10 | 2012-11-15 | Hitachi, Ltd. | Slide bearing device and compressor |
US9255606B2 (en) * | 2009-12-10 | 2016-02-09 | Hitachi, Ltd. | Slide bearing device and compressor |
CN103302293A (en) * | 2013-05-24 | 2013-09-18 | 淮海工学院 | Spray deposition densifying device and application thereof |
CN103302293B (en) * | 2013-05-24 | 2014-12-17 | 淮海工学院 | Spray deposition densifying device and application thereof |
Also Published As
Publication number | Publication date |
---|---|
GB1417244A (en) | 1975-12-10 |
DE2402382A1 (en) | 1974-07-25 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US3428374A (en) | Self-lubricating bearing | |
US8205891B2 (en) | Intershaft seal assembly | |
CN107816370B (en) | Hydrodynamic plain bearings and turbochargers | |
US3948533A (en) | Composite ring made of press fitted parts and method of assembling | |
US3561829A (en) | Means for maintaining the clearance in rolling bearings | |
US5626347A (en) | Coning resistant face seal having a "U" shape | |
US7329048B2 (en) | Self contained squeeze film damping system | |
US3201183A (en) | Shaft and sliding bearing assembly | |
US3942847A (en) | Temperature compensating ceramic metal bearing systems | |
US4145058A (en) | Shaft seal assembly for high speed and high pressure applications | |
EP0922891A2 (en) | Rotary, reciprocating seals with internal metal band | |
US3084003A (en) | Press fitted sleeves | |
US4808070A (en) | Fluid bearing | |
US5380112A (en) | Assembly for concentrically positioning a casing relative to a shaft | |
US5577847A (en) | Supporting arrangement for a bearing in an electric motor | |
US10330145B2 (en) | Gear pump bearing | |
US3535006A (en) | Bearing construction | |
GB464028A (en) | Improvements in or relating to bearings and method of lubricating same | |
US5544896A (en) | Composite face seal | |
US20190234240A1 (en) | Non-contacting seal with non-abradable coating | |
US5310265A (en) | Axially fed hydrostatic bearing/seal | |
US6017592A (en) | Process for the manufacture of a tribo-system | |
US5562349A (en) | Bearing assembly having thermal compensation | |
US3830552A (en) | Journal bearings | |
EP0549751B1 (en) | Preloaded assembly with thermal compensation |